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Anti-icing system for aircraft 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-021/04
출원번호 US-0458847 (1989-12-29)
발명자 / 주소
  • Rudolph Peter K. C. (Seattle WA) Georgefalvy Dezso (Mercer Island WA)
출원인 / 주소
  • The Boeing Company (Seattle WA 02)
인용정보 피인용 횟수 : 81  인용 특허 : 0

초록

An anti-icing system for leading edges of an aircraft. Hot compressed air is discharged from a cavity behind the leading edge, through a multitude of small holes in the leading edge skin into the airflow impinging on the leading edge. In a first embodiment the anti-icing system utilizes part of the

대표청구항

An anti-icing apparatus for an aircraft, said apparatus comprising: a. an aircraft structure comprising a skin section with a leading edge and with a first forwardly facing leading edge surface portion which is that portion of said skin section most susceptible to icing, and a second surface portion

이 특허를 인용한 특허 (81)

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